• Title/Summary/Keyword: HILS Test

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Hardware-in-the-loop Simulation Method for a Wind Farm Controller Using Real Time Digital Simulator

  • Kim, Gyeong-Hun;Kim, Jong-Yul;Jeon, Jin-Hong;Kim, Seul-Ki;Kim, Eung-Sang;Lee, Ju-Han;Park, Minwon;Yu, In-Keun
    • Journal of Electrical Engineering and Technology
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    • v.9 no.5
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    • pp.1489-1494
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    • 2014
  • A hardware-in-the-loop simulation (HILS) method for a wind farm controller using a real time digital simulator (RTDS) is presented, and performance of the wind farm controller is analyzed. A 100 MW wind farm which includes 5 MW wind power generation systems (WPGS) is modeled and analyzed in RSCAD/RTDS. The wind farm controller is implemented by using a computer, which is connected to the RTDS through transmission control protocol/internet protocol (TCP/IP). The HILS results show the active power and power factor of the wind farm, which are controlled by the wind farm controller. The proposed HILS method in this paper can be effectively utilized to validate and test a wind farm controller under the environment in practice without a real wind farm.

Worst-case Development and Evaluation for Vehicle Dynamics Controller in UCC HILS (차량자세제어 최악상황 개발 및 UCC HILS 시스템 기반 성능 평가)

  • Kim, Jin-Yong;Jung, Do-Hyun;Jeong, Chang-Hyun;Choi, Hyung-Jeen
    • Transactions of the Korean Society of Automotive Engineers
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    • v.19 no.6
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    • pp.30-36
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    • 2011
  • The current test methods are insufficient to evaluate and ensure the safety and reliability of vehicle system for all possible dynamic situation including the worst case such as rollover, spin-out and so on. Although the known NHTSA Sine with dwell steering maneuvers are applied for the vehicle performance assessment, they aren't enough to estimate other possible worst case scenarios. Therefore, it is crucial for us to verify the various worst cases including the existing severe steering maneuvers. This paper includes useful worst case based upon the existing worst case scenarios mentioned above and worst case evaluation for vehicle dynamic controller in simulation basis and UCC HILS. The only human steering angle is selected as a design parameter here and optimized to maximize the index function to be expressed in terms of both yaw rate and side slip angle. The obtained scenarios were enough to generate the worst case to meet NHTSA worst case definition. It has been concluded that the new procedure in this paper is adequate to create other feasible worst case scenarios for a vehicle dynamic control system.

A Simulation Technique of the Shipboard INS Transfer Alignment Environments using Hardware-In-the-Loop Simulation (HILS를 이용한 함정의 관성항법장치 전달정렬 환경 모의 기법)

  • Kim, Woon-Sik;Yang, Tae-Soo;Kim, Sang-Ha
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.2
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    • pp.181-188
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    • 2011
  • A simulation technique, which simulate dynamic motion and communication environments of ship in the lab, is needed in order to reduce the testing cost when we evaluate the transfer alignment performance of shipboard INS. Hardware-In-the-Loop Simulation(HILS) can be used as an effective test method for those system because it can provide flexible and realistic simulation environments, various test scenario, and repeated test environment in the lab without additional cost and person. This paper presents the methods for implementing the real time HILS environment for testing transfer alignment performance of shipboard INS. It includes real time executive for controlling realtime simulation and calculating the ship motion, communication method for interfacing between the systems, and coordinate transformation method for converting real ship coordinate attitude data to lab coordinate attitude data.

Assessment of Flight Control Performance based on the Ground Test Results of Smart UAV (스마트 무인기의 지상시험을 통한 비행제어 성능분석)

  • Kang, Young-Shin;Park, Bum-Jin;Yoo, Chang-Sun;Kim, Yu-Shin;Koo, Sam-Ok
    • Aerospace Engineering and Technology
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    • v.9 no.1
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    • pp.1-8
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    • 2010
  • The tilt-rotor Smart UAV(Unmanned Air Vehicle) has been developed by KARI(Korea Aerospace Research Institute) for civil purposes. In order to prove the reliabilities of total system of Smart UAV, the series of ground tests were performed including system interface test, aircraft HILS(Hardware In the Loop Simulation) Test, ground power test, 4-DOF (Degrees of Freedom)rig test, and tethered hover test. Many unexpected problems occurred at each ground test. With clearing these problems, the total Smart UAV systems were matured and the airworthiness was proven enough. After complete of additional ground test proposed by FRRB(Flight Readiness Review Board), the first flight test will be performed in this year. This paper presents the procedures and the analysis results of the ground tests for the tilt-rotor Smart UAV.

Implementation of Two TMS320F28335 based BESS Controllers for Microgrid and Control Performance Test in the Hardware-in-the-Loop Simulation System (마이크로그리드용 2기의 TMS320F28335 기반 BESS 제어기 구현 및 Hardware-in-the-Loop Simulation 시스템을 이용한 제어 성능 테스트)

  • Kim, Nam-Dae;Yoo, Hyeong-Jun;Kim, Hak-Man
    • The Transactions of The Korean Institute of Electrical Engineers
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    • v.63 no.4
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    • pp.559-564
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    • 2014
  • A microgrid as a small scale power system is operated by the grid-connected mode and islanded mode. It is anticipated that the battery energy storage system (BESS) is able to be applied to the microgrid for stable power control, such as tie-line and smoothing control in the grid-connected mode and voltage and frequency control in the islanded mode. In this paper, a digital signal processor (DSP), Two BESS controllers based on TMS320F28335 of a microgrid are implemented and are tested to show control performance in the hardware-in-the loop simulation (HILS) system.

Emulation of Variable Wind Speed and Turbulance Effect in a Wind Turbine Simulator (가변 풍속과 터뷸런스를 고려한 가변속 풍력 발전 시스템 시뮬레이터 개발)

  • Song, Seung-Ho;Kim, Dong-Yong;Kim, In-Sun;Kyong, Nam-Ho
    • 한국신재생에너지학회:학술대회논문집
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    • 2006.11a
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    • pp.290-296
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    • 2006
  • Control algorithms and implementation issues for a wind turbine simulator are presented for realistic emulation of variable wind characteristics using a lab-scale motor and generator set. When the average wind speed nd turbulence level is given, the torque reference of prime mover is decided through various blocks, such as random wind speed generator, blade characteristic curves, and tower effect compensation. The variable nature of wind can be implemented and tested by not only the computer simulation but also the hardware-in-loop-simulator (HILS). Some application examples of HILS include the development and test of turbine control software for more efficient and stable operation. Feasibility of the proposed simulator has verified by computer simulations and experiment.

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HILS Technique based on Inertial Sensor Modeling for High Maneuvering Missiles (고기동 유도탄 모의비행시험 기법 밀 관성센서 모델링)

  • Kim, Ki-Seung;Yu, Myeong-Jong;Ra, Won-Sang;Lee, Sang-Woo;Kim, Young-Ju
    • Proceedings of the KIEE Conference
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    • 2005.07d
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    • pp.2540-2542
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    • 2005
  • This paper proposed the new HILS technique called Injection Method for Inertial Sensor Verification of high maneuvering missiles. The performance of Inertial Sensor is verified by Injection Method and traditional FMS Method. After all, Injection Method for Inertial Sensor has capability for various scenario and critical condition test.

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Development of Dynamic Modeling and Control Algorithm for Lateral Vibration HILS of Railway Vehicle (철도 차량 횡진동 HILS를 위한 동적 모델링 및 제어 알고리즘 개발)

  • Lee, Jae-Ha;Kwak, Moon-K.;Yang, Dong-Ho;You, Won-Hee
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.22 no.7
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    • pp.634-641
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    • 2012
  • This paper is concerned with the dynamic modeling for the hardware-in-the-loop simulation of lateral vibrations of a railway vehicle. The resulting dynamic model is a nine degree-of-freedom model which can describe the lateral, roll and yaw motions of the car body and two bogies. It is assumed that the external disturbances come from wheel motions. In order to test the efficacy of the model, the linear quadratic regulator and the sky-hook control algorithm were designed and applied to the model. The simulation results show that both control algorithms are effective in suppressing the vibrations of railway vehicles.

Design and Performance Test of Controller of Interlinking Converter in AC/DC Microgrid in Hardware-in-the-Loop Simulation Environment (HILS 환경에서 AC/DC 마이크로그리드의 연계 컨버터 제어기 설계 및 테스트)

  • Ji, Hyeon-Kyun;Yoo, Hyeong-Jun;Kim, Hak-Man;Lee, Byeong-Ha
    • Proceedings of the KIEE Conference
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    • 2015.07a
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    • pp.527-528
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    • 2015
  • 최근 다양한 디지털기기에 따른 DC 부하의 증가와 함께 기존 배전망과 연계하여 운용할 수 있는 AC 그리드와 태양광과 연료전지 같은 DC 전원에 직접적으로 연계하여 운용하는 DC 그리드를 통합하는 AC/DC 마이크로그리드에 대한 연구가 진행되고 있다. 본 논문에서는 AC 그리드와 DC 그리드를 연계 제어하는 연계(interlinking) 컨버터의 제어기를 설계하고 성능을 검토하기 위해 TMS320F28335 DSP(Digital Signal Processor)와 실시간 디지털 시뮬레이터인 eMEGAsim으로 구성된 HILS(Hardware-in-the-Loop Simulation) 시스템을 구축하고 설계된 제어기의 성능을 테스트하였다.

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The Development of The Simulation Environment for Operating a Simultaneous Man/Unmanned Aerial Vehicle Teaming (유/무인 항공기 복합운용체계 검증을 위한 시뮬레이션 환경 구축)

  • Gang, Byeong Gyu;Park, Minsu;Choi, Eunju
    • Journal of Aerospace System Engineering
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    • v.13 no.6
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    • pp.36-42
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    • 2019
  • This research illustrates how the simulation environment for operating the simultaneous man/unmanned aerial vehicle teaming is constructed. X-Plane program, HILS for the ducted fan aircraft (unmanned) and CTLS (manned aircraft) with communication devices are interfaced to simulate the basic co-operational flight. The X-plane and HILS can allow operators to experience the maned and unmanned aircraft operation in the airspace on the ground in turn they can perform various simulated missions in advance before the actual flight. For the test purpose, the data link between man/unmanned aircraft and ground control station is examined using C Band and UHF radio channels by the manned aircraft.